CN217571721U - A head assembly for screw machine - Google Patents

Abstract

The utility model discloses a head assembly for screw machine, including the headstock, the mid-mounting of headstock has the aircraft nose, and the mid-mounting of aircraft nose has the mount, the bolt is worn to be equipped with in the both sides of mount, locating component is installed to the bottom of aircraft nose, the joint frame is installed to the rear end of headstock, and the rear end of joint frame is connected with the mounting panel, can fix a position back use with it through locating component, the locating frame can support the aircraft nose, prevent because the impact force, lead to the aircraft nose dislocation condition to appear, through the use impact force of the reducible aircraft nose of spring assembly, the rear end of headstock is connected with the joint frame, the mounting hole has all been seted up to the middle part and the lower extreme of joint frame, can install lubricating component in the mounting panel of joint frame, assemble, lubricating component's lubrication bottle and oil drain pipe wear to establish in the mounting hole of the middle part and the lower extreme of joint frame, can lubricate the processing to the slip region, prevent that the aircraft nose from putting up in gliding in-process, the phenomenon that the card appears.

Description

A head assembly for screw machine

Technical Field

The utility model relates to a screw machine field especially relates to a head assembly for screw machine.

Background

The screw machine is a small machine for automatically locking screws, and the action structure of the screw machine can be generally divided into a feeding part and an electric screwdriver part, wherein the feeding part is responsible for screening and providing screws, the electric screwdriver part is responsible for taking and locking the screws, and the generation of the screw machine not only improves the operation efficiency, but also reduces the manual operation intensity.

When the head assembly of the existing screw machine is used, the head assembly is difficult to position and then used, and the head frame is easy to clamp and pause at the position of a track in the moving process.

SUMMERY OF THE UTILITY MODEL

In order to overcome the defects of the prior art, the utility model provides a head assembly for screw machine, convenient and efficient carry out the adaptation installation to head assembly.

In order to solve the technical problem, the utility model provides a following technical scheme: the utility model provides a head assembly for screw machine, includes the headstock, the mid-mounting of headstock has the aircraft nose, and the mid-mounting of aircraft nose has the mount, the bolt is worn to be equipped with in the both sides of mount, locating component is installed to the bottom of aircraft nose, the joint frame is installed to the rear end of headstock, and the rear end of joint frame is connected with the mounting panel, lubricated subassembly has been inserted to the middle part ann of mounting panel.

As a preferred technical scheme of the utility model, locating component includes locating rack, spring assembly and fixed screw, and locating component's mid-mounting has the locating rack, spring assembly is installed to the bottom of locating rack, fixed screw is worn to be equipped with on the top of locating rack.

As a preferred technical scheme of the utility model, the locating rack passes through spring assembly and fixed screw constitution elastic construction, be fixed connection between locating rack and the fixed screw.

As a preferred technical scheme of the utility model, lubricated subassembly is including smooth bottle and row oil pipe, and lubricated subassembly's mid-mounting has lubricated bottle, the inner wall connection of lubricated bottle has row oil pipe.

As an optimal technical scheme of the utility model, be fixed connection between lubricated bottle and the oil extraction pipe, the oil extraction pipe is L font structure.

As an optimal technical scheme of the utility model, be fixed connection between mount and the bolt, the bolt is about the central symmetric distribution of mount.

As an optimal technical scheme of the utility model, for closely laminating between lubricated subassembly and the mounting panel, lubricated subassembly is provided with two sets ofly.

Compared with the prior art, the utility model discloses the beneficial effect that can reach is:

1. the utility model is provided with the positioning component, the positioning component can be used after positioning, the positioning frame can support the machine head, the machine head is prevented from being dislocated due to impact force, the using impact force of the machine head can be reduced through the spring group, the fixing screw is arranged at the bottom end of the machine head in a penetrating way, and the positioning frame can be effectively locked;

2. the utility model discloses a be provided with lubricating assembly, wear to establish in the middle part of joint frame and the mounting hole of lower extreme through lubricating assembly's lubricated bottle and oil drain pipe, can lubricate the processing to the slip region, prevent that the aircraft nose frame from at gliding in-process, the phenomenon that the card went up appears.

Drawings

Fig. 1 is a schematic side view of the headstock of the present invention;

FIG. 2 is a bottom view of the head frame of the present invention;

FIG. 3 is an enlarged structural view of the point A in FIG. 2 according to the present invention;

fig. 4 is a right view structural diagram of the headstock of the present invention.

Wherein: 1. a headstock; 2. a machine head; 3. a fixed mount; 4. a bolt; 5. a positioning assembly; 501. a positioning frame; 502. a spring set; 503. a fixing screw; 6. a clamping frame; 7. mounting a plate; 8. a lubrication assembly; 801. a lubrication bottle; 802. an oil discharge pipe.

Detailed Description

In order to make the technical means, the creation features, the achievement purposes and the functions of the invention easy to understand, the invention is further explained below with reference to the specific embodiments, but the following embodiments are only the preferred embodiments of the invention, not all. Based on the embodiments in the embodiment, those skilled in the art can obtain other embodiments without making creative efforts, and all of them belong to the protection scope of the present invention. The experimental methods in the following examples are conventional methods unless otherwise specified, and materials, reagents and the like used in the following examples are commercially available unless otherwise specified.

The embodiment is as follows:

as shown in fig. 1-4, the utility model provides a head assembly for screw machine, including headstock 1, the mid-mounting of headstock 1 has aircraft nose 2, and the mid-mounting of aircraft nose 2 has mount 3, and bolt 4 is worn to be equipped with by the both sides of mount 3, and locating component 5 is installed to the bottom of aircraft nose 2, and joint frame 6 is installed to the rear end of headstock 1, and the rear end of joint frame 6 is connected with mounting panel 7, and lubricated subassembly 8 has been inserted in the middle part of mounting panel 7.

Firstly, install aircraft nose 2 in the middle part of headstock 1, intercept aircraft nose 2 through mount 3, prevent the condition that aircraft nose 2 from dropping, insert in aircraft nose 2's both sides through bolt 4, just can lock aircraft nose 2 in headstock 1, install locating component 5 through the bottom of headstock 1, prevent aircraft nose 2 when using, the condition that prevents the dislocation appears, can use after fixing a position it through locating component 5, locating rack 501 can support aircraft nose 2, prevent because the impact force, lead to aircraft nose 2 the dislocation condition to appear, can reduce the use impact force of aircraft nose 2 through spring assembly 502, wear to establish fixed screw 503 in aircraft nose 2 bottom, can effectually lock locating rack 501, locating rack 501 is located aircraft nose 2's both sides, can fix a position aircraft nose 2 and lock, the rear end of headstock 1 is connected with joint frame 6, the middle part and the lower extreme of joint frame 6 have all seted up the mounting hole, can install lubrication assembly 8 in mounting panel 7 of joint frame 6, lubricate, wear to establish in the mounting hole of middle part and the lower extreme of joint frame 6 through lubrication assembly 8 and oil drain pipe 802, can handle the phenomenon in the mounting hole of lubrication area of headstock, prevent the phenomenon that the slip region 1 from appearing in the slip region, the lubricating assembly process.

In other embodiments, the positioning assembly 5 includes a positioning frame 501, a spring set 502 and a fixing screw 503, the positioning frame 501 is installed in the middle of the positioning assembly 5, the spring set 502 is installed at the bottom end of the positioning frame 501, the fixing screw 503 is installed at the top end of the positioning frame 501 in a penetrating manner, the positioning frame 501 forms an elastic structure with the fixing screw 503 through the spring set 502, and the positioning frame 501 is fixedly connected with the fixing screw 503.

Through being provided with locating component 5, can fix a position the back through locating component 5 and use it, locating rack 501 can support aircraft nose 2, prevents because the impact force, leads to the dislocation condition to appear in aircraft nose 2, and the use impact force of reducible aircraft nose 2 through spring assembly 502 wears to establish fixing screw 503 in aircraft nose 2 bottom, can effectually lock locating rack 501.

In other embodiments, the lubricating assembly 8 includes a sliding bottle 801 and an oil drain pipe 802, the lubricating bottle 801 is installed in the middle of the lubricating assembly 8, the oil drain pipe 802 is connected to the inner wall of the lubricating bottle 801, the lubricating bottle 801 and the oil drain pipe 802 are fixedly connected, and the oil drain pipe 802 is of an L-shaped structure.

Through being provided with lubricating assembly 8, wear to establish in the mounting hole of the middle part and the lower extreme of joint frame 6 through lubricating assembly 8's lubricated bottle 801 and oil drain pipe 802, can lubricate the region that slides, prevent that headstock 1 from at gliding in-process, the phenomenon that the card is pause appears.

In other embodiments, the fixing frame 3 is fixedly connected with the bolts 4, the bolts 4 are symmetrically distributed about the center of the fixing frame 3, the lubricating assemblies 8 are tightly attached to the mounting plate 7, and the lubricating assemblies 8 are arranged in two groups.

The rear end through headstock 1 is connected with joint frame 6, and the mounting hole has all been seted up to the middle part and the lower extreme of joint frame 6, can install lubricating assembly 8 in the mounting panel 7 of joint frame 6, assembles.

In the present disclosure, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may comprise direct contact between the first and second features, or may comprise contact between the first and second features not directly. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. "beneath," "under" and "beneath" a first feature includes the first feature being directly beneath and obliquely beneath the second feature, or simply indicating that the first feature is at a lesser elevation than the second feature.

The foregoing shows and describes the general principles, essential features, and advantages of the invention. It should be understood by those skilled in the art that the present invention is not limited by the above embodiments, and the description in the above embodiments and the description is only preferred examples of the present invention, and is not intended to limit the present invention, and that the present invention can have various changes and modifications without departing from the spirit and scope of the present invention, and these changes and modifications all fall into the scope of the claimed invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (7)

1. A head assembly for a screw machine, comprising a head frame (1), characterized in that: the utility model discloses a quick-witted, including head frame (1), and the middle part of head frame (1) installs aircraft nose (2), and the mid-mounting of aircraft nose (2) has mount (3), bolt (4) are worn to be equipped with by the both sides of mount (3), locating component (5) are installed to the bottom of aircraft nose (2), joint frame (6) are installed to the rear end of head frame (1), and the rear end of joint frame (6) is connected with mounting panel (7), lubricating component (8) have been inserted to the middle part ann of mounting panel (7).

2. A head assembly for a screw machine as claimed in claim 1, wherein: locating component (5) include locating rack (501), spring assembly (502) and set screw (503), and the mid-mounting of locating component (5) has locating rack (501), spring assembly (502) are installed to the bottom of locating rack (501), set screw (503) are worn to be equipped with on the top of locating rack (501).

3. A head assembly for a screw machine as claimed in claim 2, wherein: the positioning frame (501) and the fixing screw (503) form an elastic structure through the spring group (502), and the positioning frame (501) is fixedly connected with the fixing screw (503).

4. A head assembly for a screw machine as claimed in claim 1, wherein: lubricating assembly (8) are including smooth bottle (801) and oil drain pipe (802), and lubricating assembly (8) mid-mounting has lubricating bottle (801), the inner wall of lubricating bottle (801) is connected with oil drain pipe (802).

5. A head assembly for a screw machine as claimed in claim 4, wherein: the lubricating bottle (801) is fixedly connected with the oil drain pipe (802), and the oil drain pipe (802) is of an L-shaped structure.

6. A head assembly for a screw machine as claimed in claim 1, wherein: the fixing frame (3) is fixedly connected with the bolts (4), and the bolts (4) are symmetrically distributed about the center of the fixing frame (3).

7. A head assembly for a screw machine as defined in claim 1, wherein: for the laminating closely between lubricated subassembly (8) and mounting panel (7), lubricated subassembly (8) are provided with two sets ofly.

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